Finding Near Earth Objects
Before They Find Us!
(and knowing what to do about it)
Lindley Johnson Near Earth Object Observations Program Executive NASA HQ
January 8, 2014
Finding Near Earth Objects Before They Find Us! (and knowing what - - PowerPoint PPT Presentation
Finding Near Earth Objects Before They Find Us! (and knowing what to do about it) Lindley Johnson Near Earth Object Observations Program Executive NASA HQ January 8, 2014 CHELYABINSK EVENT February 15, 2013 17-20 meter object ~500-550
January 8, 2014
4
The Director of OSTP will: (1) develop a policy for notifying Federal agencies and relevant emergency response institutions of an impending near-Earth object threat, if near-term public safety is at risk; and (2) recommend a Federal agency or agencies to be responsible for –
(A) protecting the United States from a near-Earth object that is expected to collide with Earth; and (B) implementing a deflection campaign, in consultation with international bodies, should one be necessary
* http://www.whitehouse.gov/sites/default/files/microsites/ostp/ostp-letter-neo-senate.pdf 5
establishes the goal of conducting a human mission to an NEO by 2025
* http://www.whitehouse.gov/the-press-office/remarks-president-space-exploration-21st-century
NASA shall: “Pursue capabilities, in cooperation with other departments, agencies, and commercial partners, to detect, track, catalog, and characterize near-Earth objects to reduce the risk of harm to humans from an unexpected impact on our planet and to identify potentially resource-rich planetary
* http://www.whitehouse.gov/sites/default/files/national_space_policy_6-28-10.pdf
“The budget request includes a doubling of NASA’s efforts to identify and characterize potentially hazardous near-Earth objects (NEOs). This increase in the budget reflects the serious approach NASA is taking to understand the risks of asteroid impacts to our home planet. It will also help identify potential targets for the future human mission to an asteroid.”
6
Within US Government:
with regard to public release of information
necessary observations, analyses, and characterization efforts have taken place to determine that a space object indeed represents a credible threat
– Depends on level of risk and urgency, may unfold for years after detection – Will entail various combinations of:
near term
7
Upon notification from NASA: Of impending NEO Threat to United States territory:
notify appropriate Federal, state and local authorities and emergency response institutions utilizing existing resources and mechanisms
– When time/location of affected areas known, activate National Warning System – Analogous to large re-entering space debris and/or hurricane warning procedures – Post-impact event, analogous to other disaster emergency and relief efforts
Of NEO Threat beyond United States territory:
minimize loss of human life and property
– Bilaterally through diplomatic channels to potentially affected countries – To member nations of multilateral forums – UN entities (OOSA, COPUOS), NATO, etc – Post-impact event, convey offers of disaster relief and technical assistance
8
– Identify potential impact hazards early – Provide as much advanced warning of impact threat to enable more mitigation options
development and not yet ready for implementation
– Wide range of possible scenarios and challenges involved – Significantly more analysis and simulation needed to understand feasibility and effectiveness
assessment of applicable technologies
– Close coordination with DOD, FEMA, and other relevant departments and agencies – Possible emergency response exercises to be led by FEMA – Outreach to relevant private-sector stakeholders to leverage related work
– Important to engage other nations and multilateral forums to explore opportunities for international cooperation, e.g. UNCOPUOS, European Union, ISECG
9
track, catalogue, and characterize the physical characteristics of near-Earth objects equal to or greater than 140 meters in diameter in order to assess the threat of such near-Earth objects to the Earth. It shall be the goal of the Survey program to achieve 90 percent completion of its near-Earth object catalogue within 15 years [by 2020].
10
(Current Systems)
MIT/LL
Soccoro, NM
UofAZ Arizona & Australia
Minor Planet Center (MPC)
www.cfa.harvard.edu/iau/mpc.html
NEO Program Office @ JPL
http://neo.jpl.nasa.gov/
Uof HI Haleakula, Maui
JPL Sun-synch LEO
11
Operations Jan 2010 Feb 2011, 129 NEAs found Reactivated Sep 2013
Start of NASA NEO Program
10,573 12/31/13
Includes 94 comets
864 12/31/13
12
13
Courtesy of Catalina Sky Survey
15 Credit Steve Chesley, NEO PO, JPL
Infrasound Detection: 3:25 UT 11.3° N 43° W
Current Spaceguard Survey Infrastructure and Process
Survey, Detect, & Report Correlate, Determine Rough Orbit Possible New PHO? Routine Processing Publish Results
Yes
Potential Impact? Resolve Result Differences Publish Results
No
Precision Orbit and Follow Up Observations Impact Still Possible? Observations and Update Orbit Publish/ Update Results
No No Yes Yes
Iterate
Survey Systems Minor Planet Center JPL NEO Office* * In parallel with NEODyS
Radar Alerts to NASA HQ
possible close approach
potential for impact
publishes probability of impact
16
~96% ~60% ~10% <1% <<1%
18
100 102 104 106 108 1010 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 10
10
2
10
5
10
8
10 102 104 106 108 0.01 0.1 1 10 Brown et al. 2002 Constant power law Discovered to 7/21/10 2010 K-T Impactor Tunguska Absolute Magnitude, H Diameter, Km N(<H) Impact Interval, years Impact Energy, MT
Population (powers of 10) 0.01 0.1 1 10
Assumes average density and 20 km/sec impact velocity Hiroshima Protected by Earth’s Atmosphere
Average Impact Interval (yrs)
100 102 104 106 108 1010 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 10
10
2
10
5
10
8
10 102 104 106 108 0.01 0.1 1 10 Brown et al. 2002 Constant power law Discovered to 7/21/10 2010 K-T Impactor Tunguska Absolute Magnitude, H Diameter, Km N(<H) Impact Interval, years Impact Energy, MT
140 m
50 m
1 km
~250,000 ~20,000 ~ 1,000
Population (powers of 10) 0.01 0.1 1 10
Assumes average density and 20 km/sec impact velocity Hiroshima Protected by Earth’s Atmosphere
Average Impact Interval (yrs)
and shape to within ~2 m, as well as rotation state.
important for estimating albedo and spectral class, and from these an approximate density can be inferred.
state.
determining the area-to-mass ratio.
assumed density, and it should be constrained by the estimate of the area-to-mass ratio. Even so, mass may only be known to within a factor of 3 or 4.
spectral class.
21
Assumed albedo ρ = 0.04 Assumed albedo ρ = 0.34
22
22
Arecibo 305 m Bennu (OSIRIS-ReX Target): Goldstone 70 m
Observations Shape Model
23
NASA InfraRed Telescope Facility (IRTF)
Spitzer Infrared Space Telescope
Observations Intermediate parameters Objectives Rough
Precise
Absolute magnitude Density Size Albedo Apparent magnitude Mass Spectral type Phase curves Colors, Spectroscopy Radar Light curves Rotation, Shape Additional astrometry Initial detection, astrometry, photometry Thermal infrared
Rough Approximation of Precise Approximate
Area/Mass Ratio Astrometry over months or years
– Initial size estimate: ~6m, Close approach 8 March at 0.5 lunar distance.
– L- or Xe-type, inferred albedo range of 0.1-0.4, density range of 2.0-3.0 g/cc – Diameter = 2.6 - 8.4 m, mass = 20 - 930 t – Spin rate ~0.5 rpm
– Diameter = 1.5 - 3 m albedo > ~0.4 – Constrains mass to < 50 t – Spin rate: 0.5 – 2 rpm
25 ¡
– NEO Observations Program mitigation effects grants – NASA Innovative Advanced Concepts Program study awards – Kinetic Impactor demonstration mission studies
– Impact Effects Studies
– Impact Emergency Response Exercises
– Newly initiated capabilities studies with DARPA and DOE National Nuclear Security Administration (NNSA)
– UN Committee on Peaceful Uses of Outer Space Scientific and Technical Subcommittee
26
Interna7onal ¡ Asteroid ¡Warning ¡ Network ¡(IAWN) ¡ Space ¡Missions ¡ Planning ¡Advisory ¡ Group ¡ (SMPAG) ¡ Impact ¡disaster ¡ planning ¡advisory ¡ group ¡
Observers, ¡analysts, ¡ modelers… ¡ Space ¡Agencies ¡ Disaster ¡response ¡ agencies ¡
COPUOS ¡
Inform ¡in ¡case ¡of ¡credible ¡threat ¡ Disaster ¡ Response ¡ ¡Plans ¡ D e fl e c <
¡ m i s s i
¡ p l a n s ¡
Ad-‑hoc ¡mi7ga7on ¡ mission ¡advisory ¡ group ¡
Advise ¡planning ¡for ¡and ¡ response ¡to ¡the ¡threat ¡
Affected ¡ na7ons ¡
E s t a b l i s h ¡ i n ¡ c a s e ¡
¡ c r e d i b l e ¡ t h r e a t ¡ See ¡A/AC.105/C.1/L.329 ¡
*hVp://www.oosa.unvienna.org/oosa/en/COPUOS/stsc/wgneo/index.html ¡
Interna7onal ¡ Asteroid ¡Warning ¡ Network ¡(IAWN) ¡ Space ¡Missions ¡ Planning ¡Advisory ¡ Group ¡ (SMPAG) ¡ Impact ¡disaster ¡ planning ¡advisory ¡ group ¡
Observers, ¡analysts, ¡ modelers… ¡ Space ¡Agencies ¡ Disaster ¡response ¡ agencies ¡
COPUOS ¡
Inform ¡in ¡case ¡of ¡credible ¡threat ¡ Disaster ¡ Response ¡ ¡Plans ¡ D e fl e c <
¡ m i s s i
¡ p l a n s ¡
Ad-‑hoc ¡mi7ga7on ¡ mission ¡advisory ¡ group ¡
Advise ¡planning ¡for ¡and ¡ response ¡to ¡the ¡threat ¡
Affected ¡ na7ons ¡
E s t a b l i s h ¡ i n ¡ c a s e ¡
¡ c r e d i b l e ¡ t h r e a t ¡ See ¡A/AC.105/C.1/L.329 ¡
*hVp://www.oosa.unvienna.org/oosa/en/COPUOS/stsc/wgneo/index.html ¡
1st ¡mee7ng ¡of ¡Steering ¡Cmte, ¡ January ¡13-‑14, ¡2014, ¡@ ¡MPC ¡ 1st ¡mee7ng ¡February ¡6-‑7, ¡ 2014, ¡hosted ¡by ¡ESA ¡@ ¡ESOC ¡
29
NASA Near-Earth Object Survey and Deflection - Analysis of Alternatives Report to Congress, March 2007 http://www.nasa.gov/pdf/171331main_NEO_report_march07.pdf NRC Report – “Defending Planet Earth: Near-Earth-Object Surveys and Hazard Mitigation Strategies”, January 2010 http://www.nap.edu/openbook.php?record_id=12842
accessible ¡NEO ¡targets ¡suitable ¡for ¡human ¡explora7on ¡in ¡a ¡7mely ¡manner. ¡ – Op7mized ¡for ¡detec7on ¡of ¡objects ¡in ¡Earth-‑like ¡orbits ¡within ¡two ¡ years ¡of ¡launch ¡ – Launch ¡ready ¡in ¡4 ¡to ¡5 ¡years ¡with ¡low ¡risk ¡
characteriza.on ¡(size, ¡rota.on ¡rate) ¡of ¡selected ¡objects. ¡
Study Description Survey Type Picture Cost NEOCam/JPL
Sweet Spot < $500 M (excluding launch)
NEOStar/BATC
Opposition ~ $500 M (excluding launch)
NEST – L2/APL
Sweet Spot < $500 M (excluding launch)
NEST - Venus/ APL
Opposition ~ $500 M (excluding launch)
32
33
Both ¡sets ¡of ¡ac7vi7es ¡leverage ¡exis7ng ¡NASA ¡work ¡while ¡amplifying ¡par7cipatory ¡engagement ¡to ¡accomplish ¡their ¡ individual ¡objec7ves ¡and ¡synergize ¡for ¡a ¡greater ¡collec7ve ¡purpose. ¡
Enhanced NEO Observation Campaign*
Asteroid Mission Grand Challenge
Robotic Mission to Redirect an Asteroid, SEP Human Mission to an Asteroid Diverse Stakeholder Engagement Mitigation Approaches Learning how to manipulate and interact with a NEA * ¡FY2014 ¡PBR ¡increases ¡NEOO ¡Program ¡to ¡$40.5M ¡
35
Asteroid Identification Segment: Ground and space based NEA target detection, characterization and selection Iden7fy ¡ Asteroid Crewed Exploration Segment: Orion and SLS based crewed rendezvous and sampling mission to the relocated asteroid Explore ¡ Asteroid Robotic Redirection Segment: Solar electric propulsion (SEP) based robotic asteroid redirect to trans-lunar space Redirect ¡
Tasked to NEOO with additional funding
36
Awareness.
covering the entire night sky every night, but not as deeply.
37
NASA InfraRed Telescope Facility (IRTF)
and Thermal Signatures. Reactivate NEOWISE
NEO Search/Characterization data collection.
NEOWISE JPL Sun-synch LEO Arecibo Observatory Goldstone Radar
Radar (Goldstone and Arecibo)
capabilities.
38
Objective: Improve the rate of detection of smaller, long synodic period NEAs. Request for Information released in October 2012 showed that several short term, affordable
Needs Addressed: Smaller hazardous NEAs, Human spaceflight target detection, orbit determination, size IR Instrument Phase A Studies:
to be hosted on commercial geosynchronous spacecraft
2015.
NEA Detector Concept (Source: Raytheon)
well as ARRM candidate targets.
the challenge is to find several that will meet the mission envelope.
within the next 2 years, both the NEO and the ARRM candidate discovery rates should at least double.
hazardous and ARRM candidates. The process has already been successfully exercised for difficult-to-characterize candidates.
interest because they provide accurate estimates of size and rotation state.
for target-of-opportunity observing time from important non-NASA facilities (eg. Subaru) can be negotiated.
has made this a rapidly expanding mission area for Planetary Science.
39